@inproceedings{21ae6c50fb724d4cb8b39eca761138f6,
title = "Calibration Technique of Torque Output Characteristic of High Dynamic Maneuvering Device on Spacecraft",
abstract = "This paper studies a torque measurement method and device for the torque output characteristics of the spacecraft maneuvering device based on the air-floating platform and explains the composition and the measurement principle under ideal conditions. The accuracy of the system is analyzed in combination with the sensor installation error. With the installation angle calibrated, system measurement error can be compensated. Finally, the effect of the installation angle compensation on the accuracy is checked with a simulation. The system measurement accuracy is better than 0.06Nm.",
keywords = "Air-floating platform, Force sensor, Maneuvering device of spacecraft, Torque characteristics",
author = "Keyu Xu and Xiaojun Chen and Xudong Li and Xianfeng Xu and Guangcheng Ma and Hongwei Xia",
note = "Publisher Copyright: {\textcopyright} 2022 Technical Committee on Control Theory, Chinese Association of Automation.; 41st Chinese Control Conference, CCC 2022 ; Conference date: 25-07-2022 Through 27-07-2022",
year = "2022",
doi = "10.23919/CCC55666.2022.9901709",
language = "英语",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "5896--5900",
editor = "Zhijun Li and Jian Sun",
booktitle = "Proceedings of the 41st Chinese Control Conference, CCC 2022",
address = "美国",
}